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Mathematical Model of Gas-Dynamic Temperature Transducer

  • V. V. KorzinEmail author
  • D. B. Melekhov
Conference paper
Part of the Lecture Notes in Mechanical Engineering book series (LNME)

Abstract

The article proposes a mathematical model of a gas-dynamic temperature transducer designed to measure the temperature of gas streams under electromagnetic and radiation fields, as well as to measure rapidly changing temperatures of gas streams with a temperature range of 20–160 °C, based on the developed models of its elements. For the development of a mathematical model, a scheme of the jet in the working chamber of the gas-dynamic temperature transducer was made. According to the physical model of the flow of the jet in the working chamber of the gas-dynamic transducer, mathematical models have been developed for the feed and receiving channels, as well as the free section of the jet in the working chamber of the gas-dynamic temperature transducer. These mathematical models for transducer elements are combined into a mathematical model of a gas-dynamic temperature transducer. The devices for which patents were obtained, developed on the basis of the mathematical models, are presented.

Keywords

Mathematical model Feed channel Receiving channel Temperature transducer Temperature meter 

References

  1. 1.
    Burkov YG, Shmelev LF, Chaplygin EI et al (1989) Jet logic elements and devices for automatic control of technological equipment. Catalog, VNIITEMR, MoscowGoogle Scholar
  2. 2.
    Zalmanzon LA, Lutsuk YuV (1969) Inkjet temperature meter. In: New in pneumonia. Science, MoscowGoogle Scholar
  3. 3.
    Bogacheva AV et al (1972) Elements and devices of jet technology. Energiya, MoscowGoogle Scholar
  4. 4.
    Vlasov II, Sultanov IT, Ziser IG (1980) Measurement of rapidly changing temperatures of gas flows by a jet-acoustic transducer. In: Methods and tools for machine diagnostics of gas turbine engines and their elements 2:242–243Google Scholar
  5. 5.
    Golovchenko AN, Kulakov MV, Shkatov EF (1974) Throttle pneumatic transducers for temperature measurement. Energy, MoscowGoogle Scholar
  6. 6.
    Gradetsky VG, Dmitriev VN (1967) On the structure of a laminar free submerged jet flowing from a capillary. Instrum Control Syst 3:5–8Google Scholar
  7. 7.
    Esaulenko NV, Kantemirov VI (2010) Experimental study of a downhole temperature sensor. Autom Telemech Commun Oil Ind 12:5–7Google Scholar
  8. 8.
    Zavaliy AA, Simbirskiy GD, Tokarev YR (1989) Adaptive reduction flow thermocouple for measuring high temperature gas flows. Methods and diagnostic tools for gas turbine engines, Kharkov, KhAI, pp 135–146Google Scholar
  9. 9.
    Goryunov VA, Dyachkov EA, Korzin VV, Telitsa SG, Chaplygin EI (2003) Development of physical quantity converters. Actual problems of design and technological support of machine-building production: mes. Report International Conference, 16–19 Sept 2003, PKK “Polytechnic”, Volgograd, pp 214–215Google Scholar
  10. 10.
    Golovchenko AN, Kulakov MV, Shkatov EF (1974) Throttle pneumatic transducers for temperature measurement. Energy, MoscowGoogle Scholar
  11. 11.
    Martashin AI (1976) Electrical parameters converters for monitoring and control systems. Energy, MoscowGoogle Scholar
  12. 12.
    Simbirsky DF, Blockages AA (1989) Contact methods for measuring high temperatures of gas flows in gas turbine engines. Methods and tools for diagnostics of gas turbine engines, KhAI, Kharkov, pp 84–104Google Scholar
  13. 13.
    Lebedev IV, Treskunov SL, Yakovenko VS (1973) Elements of inkjet automation. Mashinostroenie, MoscowGoogle Scholar
  14. 14.
    Korzin VV (2007) Theoretical analysis of the workflow jet pulsed temperature transducer. Izv. VSTU. Ser. Progressive Technol in Mech Eng 3(4):46–47Google Scholar
  15. 15.
    Levin VS, Belash VA, Karev VA, Shirokov AM (1986) Methods for designing elements of jet automation. Yablonna-86: Sat. report International conference on pneumatic and hydraulic devices and control systems, Moscow, pp 7–9Google Scholar
  16. 16.
    The Chemist’s Handbook (1966) vols I–V, 2nd edn., Chemistry, Moscow, LeningradGoogle Scholar
  17. 17.
    Chaplygin EI, Dyachkov EA, Goryunov VA, Korzin VV (2005) Jet pulse temperature sensor. Patent of Russia №2248541, bull. 8Google Scholar
  18. 18.
    Chaplygin EI, Goryunov VA, Korzin VV (2009) Jet differentiating device. Patent of Russia №88465, bull. No. 31Google Scholar
  19. 19.
    Goryunov VA, Korzin VV (2011) Jet pulse generator. Patent of Russia №107830, bull. 24Google Scholar
  20. 20.
    Korzin VV (2007) Experimental studies of the jet pulsed temperature transducer. Izv. VSTU. Ser. Progressive technologies in mechanical engineering 3(4):47–49Google Scholar

Copyright information

© Springer Nature Switzerland AG 2020

Authors and Affiliations

  1. 1.Volzhsky Polytechnical Institute (Branch) of Volgograd State Technical UniversityVolzhsky, Volgograd regionRussia
  2. 2.Ltd. “NPO Poliplast”Volzhsky, Volgograd regionRussia

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